JP2000136728A - Rotary piston engine - Google Patents

Rotary piston engine

Info

Publication number
JP2000136728A
JP2000136728A JP11331734A JP33173499A JP2000136728A JP 2000136728 A JP2000136728 A JP 2000136728A JP 11331734 A JP11331734 A JP 11331734A JP 33173499 A JP33173499 A JP 33173499A JP 2000136728 A JP2000136728 A JP 2000136728A
Authority
JP
Japan
Prior art keywords
rotor
crankshaft
exhaust
hole
crank
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP11331734A
Other languages
Japanese (ja)
Inventor
Noriaki Yoshida
徳明 吉田
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP11331734A priority Critical patent/JP2000136728A/en
Publication of JP2000136728A publication Critical patent/JP2000136728A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons
    • F02B57/08Engines with star-shaped cylinder arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B75/22Multi-cylinder engines with cylinders in V, fan, or star arrangement
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/16Engines characterised by number of cylinders, e.g. single-cylinder engines
    • F02B75/18Multi-cylinder engines
    • F02B2075/1804Number of cylinders
    • F02B2075/1808Number of cylinders two

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Valve-Gear Or Valve Arrangements (AREA)

Abstract

PROBLEM TO BE SOLVED: To obviate intake/exhaust valves, to reduce weight and size, and to realize high torque by forming the optional number of cylinders in the radial direction in a rotor, and continuously connecting pistons fitted to and installed in the respective cylinders to a crankshaft extending by penetrating through the rotor. SOLUTION: Hollow rotor shafts 2, 3 are integrally formed in a rotor 1, the optional number of cylinders 4, 5 are formed in the radial direction, and pistons 6, 7 in the respective cylinders 4, 5 are continuously connected through connecting rods 11, 12 to cranks 9, 10 of a crankshaft 8 penetratingly supported by the rotor shafts 2, 3. This rotor 1 is rotatably housed in a housing 13 for forming a suction hole 14, spark plugs 16, 17 and an exhaust hole on the periphery. A bevel gear 22 arranged in an end part of the rotor shaft 3 facing in a beval gear chamber is meshed so as to interlock with a beval gear 23 on the crankshaft 8 through beval gears 24, 25 to perform four strokes by single rotation of the crankshaft 8 and the rotor 1 to generate motive power.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は圧縮機構を形成する
ものであり、レシプロ式とロータリー式の組合わせによ
るロータリーピストンエンジン装置に関するものであ
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a rotary piston engine device which forms a compression mechanism and which is a combination of a reciprocating type and a rotary type.

【0002】[0002]

【従来の技術】自動車において、ハイテク技術により目
覚ましい発展をとげているがエンジン自体の基本構造は
そのままである。よって従来のレシプロ式エンジンは吸
気、排気のガス交換の構造がバルブ機構になっているた
め、バルブの大きさ、位置、数、熱。あるいは作動のタ
イミング等により制約を受けるため、ガス交換が著しく
阻害されるのが最大の欠点である。その欠点は次のよう
になる。 、構造が複雑で高価である。、バルブ機構の制約か
ら吸気、排気が阻害されエネルギーの損失になる。、
バルブの開閉タイミングにオーバーラップがあり気密も
れによるエネルギーの損失になる。、多気筒の排気管
の集合により排気干渉によるエネルギーの損失になる。
、バンケル、ロータリーエンジンは軽量、コンパクト
高出力で水素エンジンの実用性に有利であるとされる
が、吸気、排気にオーバーラップがあり気密もれによる
エネルギーの損失と、燃費が悪い、低速トルクが弱いと
されている。
2. Description of the Related Art In automobiles, remarkable progress has been made by high-tech technology, but the basic structure of the engine itself remains unchanged. Therefore, in the conventional reciprocating engine, the structure of the gas exchange between the intake and exhaust is a valve mechanism, so the size, position, number, and heat of the valve. Alternatively, the biggest disadvantage is that gas exchange is significantly impaired because the operation is restricted by the timing of operation. The disadvantages are as follows. , The structure is complicated and expensive. In addition, intake and exhaust are hindered by the restriction of the valve mechanism, resulting in energy loss. ,
There is an overlap in the opening and closing timing of the valve, resulting in energy loss due to airtightness. As a result, the collection of multi-cylinder exhaust pipes causes energy loss due to exhaust interference.
, Wankel and rotary engines are said to be lightweight, compact and have a high output, which is advantageous for the practicality of hydrogen engines.However, there is overlap in intake and exhaust, energy loss due to airtightness, poor fuel economy, low speed torque. It is considered weak.

【0003】[0003]

【発明が解決しようとする課題】自動車の増産と大型化
に伴い、排気ガス、特に二酸化炭素による公害で自然破
壊と地球温暖化が進み、低公害車の開発が世界的緊急課
題になっている。関係者によって対策が進められ、新し
い低公害車のバッテリーカー、ソーラーカー、水素エン
ジン車等も開発されているが、価格と実用性に問題があ
り、大きな効果がないのが現状である。
With the increase in the production and the size of automobiles, natural destruction and global warming due to pollution by exhaust gas, especially carbon dioxide, are progressing, and development of low-emission vehicles has become a global urgent issue. . Countermeasures are being taken by stakeholders, and new low-emission vehicles such as battery cars, solar cars, and hydrogen engine cars have been developed. However, there is a problem in price and practicality, and there is currently no significant effect.

【0004】本発明は、以上のような事項を解決するた
めに、簡単な機構にして、吸気、排気等のバルブとオー
バーラップ等を全部なくすることにより、独立した工程
を作り更に、各工程に適した温度管理がしやすくするこ
とにより、新しい低公害車エンジンの開発を目的とした
装置である。
[0004] In order to solve the above problems, the present invention provides a simple mechanism and eliminates all the overlaps with valves for intake and exhaust, etc., thereby forming independent processes. The purpose of this device is to develop a new low-emission vehicle engine by making it easier to control the temperature suitable for the vehicle.

【0005】[0005]

【課題を解決するための手段】上記の目的を達成するた
めに、Aのローターに中空の回転軸2、3を固着して、
任意数のシリンダー4、5(ここでは2個のシリンーダ
ー)を設け、シリンダーにピストン6、7を設け中空の
回転軸8にクランク軸を貫通して設け、クランク9、1
0、にコンロット、11、12で回転可能に連結して設
ける。Bのハウジング13に回転軸受け孔を設け、周辺
に吸入孔14、吸入助孔15、点火プラグ16、17、
排気孔18、排気助孔19、ベベルギヤー受け軸20、
21、を設けてローターとベベルギヤーを回転可能に包
み込む。
In order to achieve the above object, hollow rotary shafts 2, 3 are fixed to the rotor A,
Arbitrary number of cylinders 4 and 5 (here, two cylinders) are provided, pistons 6 and 7 are provided in the cylinder, hollow rotary shaft 8 is provided through the crankshaft, and cranks 9 and 1 are provided.
0, and are connected so as to be rotatable in con-lots, 11 and 12. A housing 13 is provided with a rotation bearing hole, and a suction hole 14, a suction auxiliary hole 15, spark plugs 16 and 17,
Exhaust hole 18, exhaust auxiliary hole 19, bevel gear receiving shaft 20,
21 to rotatably enclose the rotor and the bevel gear.

【0006】A、ローターは真円で円筒状であり、中空
のローター軸2、3を備えローター軸を中心にして回転
する。回転軸を中心にして、ローターの周辺に2個のシ
リンダー4、5を図3のようにO−P線上の上方を0度
(と360度)にして、下方の180度に異平面に放射
状に備えて(ここでは2個)、この位置を吸入工程と爆
発工程の起点とする。Q−R線上位置Qを90度、R位
置を270度として、左廻りの圧縮工程と排気工程の起
点とする。中空のローター軸の中にクランク軸8を備え
クランク9、10、にコンロット11、12、ピストン
6、7を備え、シリンダー4、5に回転可能に組み付け
て、ローター軸にベベルギヤー22、クランク軸にベベ
ルギヤー23を固着して設けている。
A, the rotor is a perfect circle and a cylindrical shape, and has hollow rotor shafts 2 and 3 and rotates about the rotor shaft. With the rotation axis as the center, the two cylinders 4 and 5 are arranged around the rotor at 0 degree (and 360 degrees) on the OP line as shown in FIG. (Here, two), this position is used as the starting point of the suction process and the explosion process. The position Q on the QR line is 90 degrees and the R position is 270 degrees, which is the starting point of the counterclockwise compression process and the exhaust process. A hollow rotor shaft is provided with a crankshaft 8 and cranks 9 and 10 are provided with conlots 11 and 12 and pistons 6 and 7 and are rotatably assembled to cylinders 4 and 5 to bevel gears 22 on the rotor shaft and a crankshaft on the rotor shaft. The bevel gear 23 is fixedly provided.

【0007】B、ハウジング13はローターを包み込む
母体で中央に回転軸受け孔を設け、周辺に各工程の気体
の流れの機構として、各工程の起点を基準にして、吸入
孔14、吸入助孔15、点火ブラグ16、17、排気孔
18、排気助孔19、ベベルギヤー受け軸20、21、
を備え、側面にはベベルギヤー室を備え、ローターとベ
ベルギヤーを包み込む。
[0007] B, the housing 13 is a mother body that encloses the rotor, has a rotary bearing hole in the center, and has a suction hole 14, a suction auxiliary hole 15 based on the starting point of each process as a mechanism of gas flow in each process. , Ignition plugs 16, 17, exhaust holes 18, exhaust auxiliary holes 19, bevel gear receiving shafts 20, 21,
It has a bevel gear chamber on the side and encloses the rotor and bevel gear.

【0008】C、4個のベベルギヤーはベベルギヤー室
のローター軸にベベルギヤー22、クランク軸にベベル
ギヤー23、を固着して備えベベルギヤー受け軸にベベ
ルギヤー24,25、が回転可能にして双方の固着ギヤ
ーと噛み合い上方矢印0度でローターのシリンダー4、
とクランク9、のピストンが共に0度になる位置の条件
で噛み合って滑合している。
C, the four bevel gears are provided with a bevel gear 22 fixed to a rotor shaft of a bevel gear chamber and a bevel gear 23 fixed to a crankshaft. At the upper arrow 0 degree, the rotor cylinder 4,
And the pistons of the crank 9 are engaged with each other under the condition that the pistons are at 0 degrees.

【0009】D、サイドハウジング26、27、はロー
ターとベベルギヤーを側面から包み込む母体でローター
軸受孔とクランク軸受孔を備えている。
D, side housings 26 and 27, which are a base body surrounding the rotor and the bevel gear from the side, have a rotor bearing hole and a crank bearing hole.

【0010】E、AのローターとCのベベルギヤーをB
のハウジングとDのサイドハウジングで回転可能に組み
付け、ベベルギヤーの噛み合い歯数比は1対1とする。
故にローター軸は左回転、クランク軸は右回転を形成す
る。
[0010] The rotor of E and A and the bevel gear of C
And the side housing of D are rotatably assembled, and the ratio of the number of meshing teeth of the bevel gear is 1: 1.
Thus, the rotor shaft forms a left rotation and the crankshaft forms a right rotation.

【0011】ローター軸とクランク軸は逆回転のためロ
ーター軸1回転とクランク軸1回転で4工程と4行程を
形成し、吸入、圧縮、爆発、排気工程を完了して、2シ
リンダーが順次4工程を形成し連続回転運動することに
より2回の爆発エネルギーを発生する。
Since the rotor shaft and the crankshaft rotate in reverse, one rotation of the rotor shaft and one rotation of the crankshaft form four steps and four strokes, and the suction, compression, explosion, and exhaust steps are completed. Two explosion energies are generated by forming a process and performing continuous rotational movement.

【0012】以上のような構造で回転軸を中心にして、
クランク軸を矢印の方向右廻りに外力でまわして、気体
の流れと各工程及びクランク軸の行程を確認してみる
と、ハウジングO−P線上の上方を0度(と360度)
の吸入工程起点として、ローター軸のシリンダー4の中
心点を矢印0度とクランク9が上死点で吸入工程0点で
クランク軸を矢印の方向右廻りに回すとシリンダーは左
廻りに回り吸入工程が始まり、少し廻り続けると混合気
は吸入孔より吸入助孔を通って流れこみ、ローターはQ
点でクランク9はR点で吸入工程と吸入行程が終わり、
With the structure as described above, with the rotation axis as the center,
Turn the crankshaft clockwise with an external force in the direction of the arrow, and check the gas flow, each process and the stroke of the crankshaft. The upper part on the housing OP line is 0 degree (and 360 degree).
As the starting point of the suction process, when the crank shaft is turned clockwise in the direction of the arrow at the point 0 at the center point of the cylinder 4 of the rotor shaft and the crank 9 at the top dead center and the crank 9 at the top dead center, the cylinder rotates counterclockwise. Begins, and when the air continues to rotate a little, the air-fuel mixture flows from the suction hole through the suction auxiliary hole, and the rotor is Q
At the point, the crank 9 finishes the suction process and the suction stroke at the point R,

【0013】同時にシリンダー5は下方位180度P点
の点火プラグから作用を受けR点に、クランク10はP
点からQ点へ爆発行程から排気行程に移動して、排気助
孔と排気孔から爆発ガス体を排出することになる。
At the same time, the cylinder 5 is acted upon by the ignition plug at the point 180 degrees P below, and the cylinder 10
Moving from point to point Q to the exhaust stroke from the explosion stroke, the explosive gas is discharged from the exhaust auxiliary hole and the exhaust hole.

【0014】更に続けてシリンダー4は爆発工程180
度P点の点火プラグ14で爆発エネルギーを受けて回転
し排気助孔と排気孔から爆発ガス体を排出する。クラン
ク9はQ点を過ぎ360度の排気完了点に向かってい
る。
Further, the cylinder 4 is operated in an explosion process 180
The ignition plug 14 at the point P receives the explosion energy and rotates to discharge the explosive gas from the exhaust auxiliary hole and the exhaust hole. The crank 9 has passed the point Q and is approaching the exhaust completion point of 360 degrees.

【0015】同時にシリンダー5はR点排気工程から0
度を過ぎて、吸入孔より吸入助孔を通って混合気体を吸
入しながら圧縮工程に向かっている。クランク10は0
点を過ぎて対抗位置R点に向かっている。更に進むと点
火プラグ15で着火爆発することになる。
At the same time, the cylinder 5 is set to 0
Exceeding the degree, it is heading to the compression process while sucking the gas mixture through the suction auxiliary hole from the suction hole. Crank 10 is 0
Passing the point, it is heading to the opposition position R point. When the ignition plug 15 proceeds further, the ignition plug 15 causes an explosion.

【0016】更に続けて2回転目、シリンダー4は36
0度の排気工程完了と同時に0度の吸入孔より吸入助孔
を通って混合気体を吸入して圧縮工程に向かっている。
クランク9は0点を過ぎR点270度の対抗位置に向か
っている。更に進むと点火プラグ14で着火爆発して2
シリンダーで180度毎にエネルギーを発生することを
特徴としたロータリーピストンエンジン装置である。
Further, the second rotation, cylinder 4 is 36
Simultaneously with the completion of the 0-degree exhaust process, the mixed gas is sucked from the 0-degree intake hole through the suction assisting hole, and the process proceeds to the compression process.
The crank 9 has passed the zero point and is heading to the opposing position at the R point of 270 degrees. If you proceed further, it ignites and explodes with spark plug 14 and 2
A rotary piston engine device that generates energy every 180 degrees in a cylinder.

【0017】[0017]

【発明の効果】本発明は、以上説明したように構成され
ているので、以下に記載されるような効果を奏する。
A、構造が簡単、軽量、コンパクト、高トルク、高馬
力、が得られる。吸、排気バルブがないため交換ガスの
制約と阻害を受けない、故にエネルギーの損失が少な
い、クランク1回転で4工程故にトルク変動が少ない
Since the present invention is configured as described above, it has the following effects.
A: A simple structure, lightweight, compact, high torque and high horsepower can be obtained. Because there is no intake and exhaust valves, there is no restriction or obstruction of the exchange gas, so there is little energy loss, and there are few torque fluctuations because there are four steps per crank rotation.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 本発明の正面図である。FIG. 1 is a front view of the present invention.

【図2】 本発明の正面図A−B−C−Dの断面図であ
る。
FIG. 2 is a sectional view of a front view ABCD of the present invention.

【図3】 本発明の図2E−F−G−H−I−Jの正面
の断面図である。
FIG. 3 is a front cross-sectional view of FIG. 2EFGGIJ of the present invention.

【符号の説明】[Explanation of symbols]

1、 ローター。 16、17 点火プラ
グ。2、3、 ローター軸。 18、 排気
孔。4、5、 シリンダー。 19、 排気
助孔。6、7、 ピストン。 20、21、
ベベルギヤー受け軸。8、 クランク軸。 2
2、23、24、25、ベベルギヤー。9、10、 ク
ランク。 26、27、 サイドハウジング。1
1、12、コンロット。13、 ハウジング。1
4、 吸入孔。15、 吸入助孔。
1. Rotor. 16, 17 spark plug. 2, 3, rotor shaft. 18. Exhaust vent. 4, 5, cylinder. 19. Exhaust auxiliary hole. 6, 7, piston. 20, 21,
Bevel gear bearing shaft. 8. Crankshaft. 2
2, 23, 24, 25, bevel gear. 9, 10, crank. 26, 27, side housing. 1
1, 12, Conlot. 13. Housing. 1
4. Suction hole. 15. Inhalation aid hole.

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 (A)、ローター(1)に中空のロータ
ー軸(2、3)と任意数のシリンダー(4、5)とシリ
ンダーにピストン(6、7)を備え、ローター軸にクラ
ンク軸(8)とクランク(9)クランク(10)にコン
ロット(11、12)を滑合して備え、(B)、ハウジ
ング(13)に回転軸受孔を備え、周辺に吸入孔(1
4)吸入助孔(15)点火プラグ(16、17)排気孔
(18)排気助孔(19)とベベルギャー受け軸(2
0、21)とベベルギャー室を備え、(C)、ベベルギ
ャー室の中空のローター軸にベベルギャー(22)クラ
ンク軸にベベルギャー(23)を固着して備え、ベベル
ギャー受け軸にベベルギャー(24、25)を備え、
(D)、サイドハウジング(26、27)にローター軸
とクランク軸受け孔を備え、(E)、AのローターとC
の、ベベルギャーをBの、ハウジングとDの、サイドハ
ウジングで組み付けて備え、上記条件でクランク軸とロ
ーターが1回転で4工程を形成することを特徴とするロ
ータリーピストンエンジン装置。
(A) A rotor (1) is provided with a hollow rotor shaft (2, 3), an arbitrary number of cylinders (4, 5), and a piston (6, 7) on a cylinder, and a crank shaft is provided on the rotor shaft. (8) and crank (9) The crank (10) is provided with sliding slots (11, 12), (B), the housing (13) is provided with rotary bearing holes, and the suction holes (1
4) Suction auxiliary hole (15) Spark plug (16, 17) Exhaust hole (18) Exhaust auxiliary hole (19) and bevel gear receiving shaft (2)
0, 21) and a bevel gear chamber. Prepared,
(D), the side housing (26, 27) is provided with a rotor shaft and a crank bearing hole, (E), the rotor of A and C
A rotary piston engine device, wherein the bevel gears are assembled with side housings of a housing B and a housing D, and the crankshaft and the rotor form four processes in one rotation under the above conditions.
JP11331734A 1999-10-17 1999-10-17 Rotary piston engine Pending JP2000136728A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11331734A JP2000136728A (en) 1999-10-17 1999-10-17 Rotary piston engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11331734A JP2000136728A (en) 1999-10-17 1999-10-17 Rotary piston engine

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP14500798A Division JPH11303643A (en) 1998-04-18 1998-04-18 Rotary piston engine and compressor

Publications (1)

Publication Number Publication Date
JP2000136728A true JP2000136728A (en) 2000-05-16

Family

ID=18247018

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11331734A Pending JP2000136728A (en) 1999-10-17 1999-10-17 Rotary piston engine

Country Status (1)

Country Link
JP (1) JP2000136728A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007534886A (en) * 2004-04-29 2007-11-29 マルチネス フランシスコ ヤビエル ルイス Balanced rotary engine
KR101175071B1 (en) * 2010-05-31 2012-08-23 김대성 Rotary piston engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2007534886A (en) * 2004-04-29 2007-11-29 マルチネス フランシスコ ヤビエル ルイス Balanced rotary engine
KR101175071B1 (en) * 2010-05-31 2012-08-23 김대성 Rotary piston engine

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